View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67839U 26145.45665501 +.00000000 +00000-0 +42144-3 0 00004
2 67839 43.0037 193.5880 0002207 262.3816 97.6785 15.27589834 09
| Epoch (UTC): | 25 May 2026 10:57:34 |
| Eccentricity: | 0.0002207 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 193.5880° |
| argument of perigee: | 262.3816° |
| revolutions per day: | 15.27589834 |
| mean anomaly at epoch: | 97.6785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|